Gas check with system for improved loading and retention in bore of muzzleloading firearms

ABSTRACT

A muzzle loading bullet gas check has external recess and ridge system, and/or an internal locking ridge system. The preferred gas check has an opening or recess on its front end for receiving and frictionally engaging a rearwardly extending post of the bullet, the opening also preferably including an internal radial ridge for gripping the post and/or locking with an indent on the post. The barrel-interacting part of the gas check has one or more external recesses and adjacent radial ridges/edges protruding relative to the recesses, which serves to reduce the total surface area of the gas check contacting the bore. The recesses do not touch the bore of the firearm, resulting in less friction and easier loading, while the outer ends/surfaces of the ridges/edges do touch the bore to retain the bullet in the bore during handling and hunting and to effectively capture gasses after the firing explosion.

This application claims benefit of priority of Patent Application Ser.No. 60/817,904, filed Jun. 30, 2006; this application is acontinuation-in-part of application Ser. No. 10/896,160, filed Jul. 20,2004, which is a continuation-in-part of application Ser. No.10/259,374, filed Sep. 27, 2002 and issued on Jul. 20, 2004 as U.S. Pat.No. 6,763,765, which is a non-provisional of Provisional Application60/325,530, filed Sep. 27, 2001; and this application is also acontinuation-in-part of application Ser. No. 11/318,076, filed Dec. 23,2005, the disclosures of all of which are incorporated herein by thisreference.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The invention relates generally to firearms, and more specifically tomuzzleloading firearms. The invention is a gas check connected to therear part of a muzzleloader projectile, or bullet, the gas checkcomprising an external radial ridge for easier loading and/or a radialinternal locking edge for better securing the gas check to theprojectile.

2. Related Art

To function most effectively, muzzle-loading firearms preferably involvethe use of a bullet in conjunction with some type of wad or gas checkmember. Throughout the history of such firearms, various configurationsthat embrace this design principle have been utilized. The wad or gascheck is used to secure the bullet properly within the bore withoutsignificant deformation of the bullet, and to prevent the escape offorward thrusting gases around the bullet upon firing the firearm. Priorto the use of wads or gas checks, a malleable lead bullet, with adiameter necessarily greater than that of the bore of the firearm, wasram-rodded down the barrel. In this manner, the bullet was frictionallysecured in place over the powder charge and engaged with the rifling ofthe bore, but was often malformed when being so placed.

The use of sabots or wrappers was later introduced to facilitate anothermechanism of securing the bullet in place in the bore of the barrel.These devices surround a sub-caliber bullet to engage the rifling andsecure the bullet without requiring the deformation of a large diameterbullet. When the firearm is discharged, the interaction between wrapperand rifling imparts spin to the bullet. C. T. James and A. Ball obtainedU.S. Pat. Nos. 34,950 and 405,690, respectively, for such wrapper-typedevices.

D. D. Williams, U.S. Pat. No. 35,273, and G. P. Ganster, U.S. Pat. No.43,017, acquired patents for inventions in which the wad was directlyattached to the bullet for use in muzzle-loading firearms.

Significant reductions in the efficiency of such firearms often resultfrom destructive interactions between the bullet and bore. When wrappersare used to surround the bullet, the positioning of the wrapper betweenthe bullet and bore may affect the ballistic qualities of the shot. Inthe case of large-diameter bullets, the scoring and deformation of theprojectile that results from the loading process may affect thedischarge of the bullet from the bore as well as the in-flightaerodynamics.

U.S. Pat. No. 5,458,064 (Kearns) discloses a gas check affixed to therear of a bullet, for the purpose of capturing and controlling theforward-thrusting gasses. The Kearns gas check is connected to thebullet by means of a pin extending from, or into a cavity of, the backof a muzzleloading, bullet. In this patent, the bullet has an outerdiameter slightly less than the inner diameter of the firearm barrel,and the gas check has an outer diameter slightly greater than the innerbarrel diameter. Kearns provides his gas check member for use withsub-caliber bullets, wherein the diameter of the gas check slightlyexceeds that of the bore. The gas check is frictionally attachedrearward of the bullet and is constructed of deformable, but durable,plastic.

U.S. Pat. No. 6,481,356 (Gualandi) discloses an enclosed projectile withexternal ridges on the enclosure for a firearm cartridge. This referencerelates to firearm cartridges, and does not relate to muzzleloadingfirearms. Also, in this reference, the enclosure separates from the sidewalls of the projectile immediately upon firing, so the enclosure doesnot interact with the projectile after firing like a sabot does.

U.S. Pat. No. 6,796,068 (Crowson et al.) also discloses a gas checksimilar to the one disclosed in U.S. Pat. No. 5,458,064, above, with theadditional feature of an expanded-shape pin at the back end of thebullet. The pin has a distal end that is larger than its proximal endthat is attached to the back of the bullet. An expanded-shape pininstalled in a round hole of the gas check provides a gap between thepin and the gas check which allows exploding gases to more easilyseparate the gas check from the bullet when desired.

U.S. Published Patent Application #2004/0079256 (McMurray et al.)discloses an enclosed projectile with interconnected collapsible finswhich create a front compressible section for a projectile from afirearm cartridge. Therefore, this reference does not relate tomuzzleloading firearms. Also, in this reference there is no disclosurethat the collapsible fins interact with the bore of the firearm afterfiring, like a gas check does.

Still, there is a need for a gas check for muzzleloading firearms thatacts to keep the bullet projectile secured in the barrel, even duringthe rigors of hunting or other handling prior to shooting the firearm.Also, there is a need for such a gas check that is easy to load,especially after the barrel has been fouled by earlier shooting. Thereis also a need for a frictionally-attached gas check for use inmuzzle-loading firearms that is preferably designed to quickly andreliably detach from the bullet and/or break apart upon firing tominimize interference by the gas check with the bullet after the bulletleaves the bore. Various embodiments of the present invention addressselected, or all, of these needs.

SUMMARY OF THE INVENTION

The present invention is a gas check for a muzzle loading projectile,herein called “bullet,” the gas check having at least one external ridgeand/or at least one internal locking ridge. Also, the present inventionmay be the combination of the instant gas check, having the externalridge and/or internal locking ridge, and the muzzle loading bullet. Thegas check is preferably a soft plastic piece, and has a forward,bullet-interacting part, and a rearward, barrel-interacting part. Thebullet-interacting part of the gas check is for connecting the frontpart of the gas check to the back part of the bullet; preferably, thisis accomplished by providing on the bullet a post extending rearwardlyto be received in and frictionally engage an aperture/opening on the gascheck front side. Preferably, this aperture/opening of the gas checkincludes, on its axial wall, an internal, radially-inwardly-extendinglocking ridge for more secure cooperation between the gas check and thepost of the bullet. The inwardly-extending ridge may abut andfrictionally engage the side surface of the pin of the bullet. There maybe one or several ridges, and, if plural, the ridges may be of the sameor different shapes and/or have different spacing between them.

The internal radial ridge(s) assist in securing the gas check to thebullet, especially when the rearwardly-extending post of the bullet hasbeen provided with a cooperating radial indent, cannelure, or retainingring. The geometry of the internal radial ridge and the cooperating ringmay be adjusted relative to each other to more securely interfit andinterconnect. Said protruding ridge(s) mating with one or moreindents/cannelures/rings, when the gas check of the preferred embodimentis connected to the bullet, serves to prevent the bullet from easilyseparating from the gas check during the loading and handling steps, andduring at least the fractions of a second after firing during which itis desirable to have the bullet and gas check connected to each other.Alternatively, a male ridge may be provided on the bullet post formating in a female indent/cannelure/ring on the gas checkaperture/opening wall surface.

The barrel-interacting part of the gas check is its outer surface thatengages the inner surface of the barrel during loading, during anyhandling, transport or hunting period before firing, and during theperiod after firing when the projectile (with gas check attached) isaccelerating down the barrel before exiting the bore. Preferably, theouter surface of the gas check has a recess and ridge system comprisingat least one radial ridge and at least one region that is recessesrelative to said ridge. There may be one or several external radialridges, and the external radial ridges, if plural, may be of the same ordifferent shapes and/or have different spacing between them.

The external radial recess and ridge system of the preferred embodimentsassists in convenient loading of the muzzle loading projectile, byminimizing resistance to the gas check being pushed into the barrel.This benefit is achieved by means of the external radial ridge(s)extending beyond the surrounding/adjacent portions of the externalsurface of the gas check for contacting the bore, with the adjacentportions of the external surface being concave or recessed relative tothe ridge(s). This ridge and recess system, therefore, provide(s) lesstotal surface area in contact with the rifle bore at all times, comparedto a smooth surface gas check. This way, there is less gas-check-on-borefriction during loading, which is especially attractive when the borehas been fouled by earlier shooting. After loading, the preferred ridgescontact the barrel and hold the gas check, with its firmly- andsecurely-connected bullet, generally centered and stable in the barreland unlikely to slide out of the barrel. Still, however, the gas checkprovides enough contact with the inside of the rifle barrel toefficiently capture exploding gases and prevent blow-by upon firing.

Preferably, said capture of gases for preventing said blow-by isaccomplished by a cup-shaped gas-capture portion formed at the rear endof the gas check. The gas-capture portion, also called a“skirt,” isgenerally axial, and it is this skirt that also provides the externalsurface comprising the preferred external recess and ridge system. Theinterior walls of the skirt tapers to be thinner towards the rear end;this way, the gas check is flexible enough at the rear end to provide,upon firing of the firearm, a good seal in the bore.

The gas check may be made rigid and durable enough at its front end toprevent excessive deformation upon explosion of the powder charge behindthe gas check; this way, the front end of the gas check is preferablyprevented from collapsing or compressing to a smaller/shorter axiallength. Also, due to the rigidity and durability of the front end, andthe security of the preferred pin (or“post”) and aperture connectionsystem, there is no need in most embodiments for any part of the gascheck to extend forward, relative to the plane of the bullet main bodyrear surface, for additional connection or gas capture or control.Further, while it is preferred that the gas check disengages from thebullet, breaks apart, or otherwise frees the bullet, at about the timeor soon after the bullet exits the barrel, said rigidity and durabilityof the front end of the gas check may be desirable as a means to preventpremature rupture or compression of the gas check during the period oftime inside the barrel when the gas check is fulfilling its purpose ofcapturing gasses and helping to propel the bullet through and out of thebarrel.

The gas check may be made with purposely-thin or otherwise weakenedportions that allow breakage or shattering of at least a portion of thegas check after the explosion, as stated above, preferably at about thetime of, or shortly after, exiting the barrel. The thinness and/or otherweakened portions (for providing said breakage or shattering at adesired time or position), are preferably not at the upper shoulders Sof the gas check, but are rather in a radial portion of the front wallthat abuts against the rear end of the bullet and/or in the skirt in aposition wherein the skirt will tend to break only upon exit of thebarrel.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A is a side, perspective view of a prior art gas check attached toa bullet.

FIG. 1B is a schematic, cross-sectional side view of one embodiment of aprior art gas check in a firearm barrel, wherein the gas check isconnected to the bullet by means of a forwardly-protruding gas check pinbeing received in a hole in the bullet.

FIG. 1C is a schematic, cross-sectional side view of another prior artgas check attached to a bullet, in the barrel of a firearm, wherein thegas check is connected to the bullet by means of a rearwardly-protrudingpin on the bullet being received in an aperture in the gas check.

FIG. 2 is a perspective view of one embodiment of the invented gas checkconnected to one embodiment of a muzzle loading firearm bullet.

FIG. 3 is a side perspective view of the gas check of FIG. 2.

FIG. 4 is a cross-sectional view of the gas check of FIGS. 2 and 3.

FIG. 5 is a bottom view of the gas check embodiment depicted in FIGS.2-4.

FIG. 6 is a cross-sectional view of the gas check depicted in FIGS. 2-5,affixed to the back of a muzzleloading bullet.

FIGS. 7A, B, C, and D is a series of cross-sectional side viewsdepicting different interfits between various embodiments of an internalridge of the gas check and various embodiments of a retaining ring onthe post of the bullet, according to several embodiments of theinvention.

FIG. 8 is a schematic illustration of one possible fragmentation of oneembodiment of the invented gas check upon leaving a firearm barrel.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

Referring to the Figures, there are depicted several, but not the only,embodiments of the present invention. In this description, “front” meansmore towards the open end of the firearm barrel, and the front end ofthe bullet and gas check are toward the open end of the barrel when thebullet and gas check combination is in the breech (or closed end) of thebarrel. “Back” means more towards the butt of the firearm, and the backend of the bullet and the gas check are toward the butt of the firearmwhen the bullet and gas check combination is in the breach.

In FIG. 1A is depicted a side, perspective view of a prior art gas checkattached to the back of a muzzleloading bullet. Such prior art gaschecks may be of the type described by Kearns in U.S. Pat. No.5,458,064, for example.

In FIG. 1B is depicted a cross-sectional side view of the prior art gascheck 10 of FIG. 1A affixed to a muzzleloading bullet 12 within firearmbarrel 14. Bullet 12 has a central hole/recess into which isfrictionally received a pin 16 that extends from the front end of gascheck 12. Outer side walls 18 of gas check 10 are uniform and smooth.All or nearly all of the outer side wall 18, all along the axial lengthof the side wall 18, contacts and interacts with the interior surface ofbarrel 14.

FIG. 1C illustrates an alternative embodiment of a prior art gas check10′ and bullet 12 combination, the outside of which appears to be thesame as the bullet and gas check combination of FIGS. 1A and 1B. Theconnection between bullet and gas check, however, is different. This gascheck 10′ has an aperture through its front, radial wall, whichfrictionally receives a pin 16′ extending rearward from the back surfaceof the bullet. This type of connection is also discussed in Kearns U.S.Pat. No. 5,458,064. Optionally, the pin extending from the back surfaceof the bullet may be of the shapes described in Crowson, et al. U.S.Pat. No. 6,796,068, for example, wherein the pin 16′ may have a distalend that is larger than its proximal end, and/or may also have gapsbetween the pin 16′ and the wall surface of the aperture receiving thepin 16′.

In FIGS. 2-6 are depicted views of one embodiment of the gas check, andsaid one embodiment of gas check combined with one embodiment of amuzzle loading firearm bullet, according to the instant invention. InFIG. 6 is depicted a schematic, cross-sectional view of the gas check 20as it is affixed to the back of a muzzle loading bullet 12. Thegenerally central aperture 28 receives a post or pin 80 on the back ofthe muzzle loading bullet 12, providing preferably a snug fit betweenthe gas check 20 and the bullet 12. While the post 80 is shown as aslightly-expanded-shape post, other pins or posts may be used, forexample, ones that are entirely cylindrical. Also, there may or may notbe one or more gaps between the post 80 outer surface and the interiorside wall surface of the gas check aperture, but significant gaps arenot preferred, as a goal of preferred embodiments of this gas check isto create a snug and secure frictional fit of the gas check to thebullet.

Gas check 20 has generally flat front surface 22, and an axial skirt 23with an external side wall surface 24 and an interior side wall surface25. Surrounding and defining aperture 28 is an axial ring 30 with a rearsurface 32, wherein said axial ring 30 is connected to the skirt 23 by athin, radial connecting ring 34. This thin, radial connecting ring 34may be made thin enough to break, after the powder explosion andpreferably immediately upon exiting the barrel allowing for freeing thebullet from the gas check so that the bullet proceeds on its flightwithout interference and without the weight of the gas check.

Side wall surface 24 is an uneven, unsmooth surface, preferablycomprising a recess and ridge system. The recess and ridge system maycomprise a combination of recessed rings separated or defined at theirboundaries by protruding circumferential ridges (or protrudingcylindrical surfaces that may still be considered thicker or broaderridges). For example, recessed circumferential rings 41, 42 or othergrooves preferably extend circumferentially around the entire side wallsurface 24. The material bordering/defining these recessed rings 41, 42are external circumferential ridges 52, 53, 56 that extend all the wayaround the gas check and protrude outward radially beyond recessed rings41, 42 may be called external ridges. The generally cylindrical surfaceregion 52 (which comprises edge 51) above the uppermost recess 41, andthe generally cylindrical surface region 56 (which comprises edge 55),may be considered smooth and cylindrical ridges or “blunt” ridges thatprotrude beyond the adjacent recesses. The ridge 53 that separates thetwo recessed rings 41, 42 is a thin, relatively sharp ridge, but,alternatively, the ridge 53 separating the two recesses 41, 42 could bebroadened so as not to be so sharp.

Some or all of the ridges/edges 52 (with edge 51), 53, and 56 (with edge55), contact the barrel surface while the bullet and gas check reside inthe barrel (during loading, hunting, and until the gas check orfragments of the gas check exit the barrel after filing). This way, thegas check provides enough surface area, spread-out appropriately alongthe axial length of the gas check, for contact with the barrel, tostabilize and center the gas check in the barrel before and preferablyafter firing and to perform its gas-check function of catching/sealingexplosion gasses from passing by the bullet. However, because asignificant amount of the side wall 24 surface area is recessed (41, 42)relative to the protruding ridges/edges 51, 52, 53, 55, 56, therecess/ridge system serves to decrease the total surface area of the gascheck in contact with the inner surface of the barrel 14 during the timethe bullet and gas check are in the barrel, thus, decreasing thegas-check-on-bore friction especially during loading.

There may be one, two, three, four, or more spaced-apart external ridgesincluded in the exterior side wall 24, including sharp ridges such asridge 53, and/or broader or flatter ridges 52, 56. Preferably, there areat least two ridges or edges extending around the skirt 23 of the gascheck (on the sides of at least one recess) that are spaced apart in theskirt axial direction (that is, higher and lower on the skirt as it isoriented in FIG. 4). A single protruding ridge, with recess on eachside, might work in some instances, however, more likely, such a singleridge would make the gas check less stable in the bore and would allowgasses to pass by the gas check, or, if the ridge were broad and therecess small, the surface area would not be reduced sufficiently to makeloading easier.

The ridges may be of the same, or different, shape and spaced the sameor differently. Typically, external ridge(s) such as the “sharp” onecall-out as 53 are between about 0.001″ and 0.006″ high (H in FIG. 4),and between about 0.001″ and 0.006″ wide (W in FIG. 4).

The recess and ridge system assists in convenient loading of themuzzleloading projectile 12, while still providing enough contact withthe inside of the rifle barrel 14 to hold the bullet in the bore duringhandling and hunting, and to efficiently capture exploding gases andprevent blow-by. The recess and ridge system provides less total surfacearea in contact with the rifle bore, compared to a smooth surface gascheck. This way, there is less gas-check-on-bore friction duringloading, which is especially attractive when the bore has been fouled byearlier shooting.

Skirt 23 forms a relatively thin-walled, rearwardly-opening, generallycylindrical portion of the gas check, which may be described as acup-shaped gas capture portion, formed at the rear end of thebullet-check combination, for gas capture upon explosion of the powdercharge behind the gas check 20. In FIG. 5 is depicted a bottom view ofthe embodiment of the preferred gas check, showing another view of thegenerally central aperture 28, and the interior wall surface 25 of theskirt 23. The external walls of the gas capture portion are generallyaxial, with the interior walls 25 of the gas capture portion alsogenerally axial but tapered so that the skirt is thinner towards therear end. This way, the gas check skirt 23 is flexible enough at itsrear end to flex, stretch, or otherwise slightly expand to provide agood seal in the bore. The gas check front end, however, is rigid anddurable enough to prevent significant deformation, compression, orshrinkage, of the gas check especially in the axial direction while ittravels through the bore.

FIG. 5A schematically depicts the muzzle loading bullet 12 connectedwith the gas check 20 by way of insertion of the bullet post 80 throughthe generally central aperture 28. Preferably, the post 80 has a smalldiameter relative to the diameter of the main body of the bullet, and itmay be said that the preferred gas check does not cover any of the mainbody of the bullet except for extending along the rear surface of themain body and surrounding the post that protrudes from the main body.Thus, the gas check connects to a relatively small protruding portion(post 80) of the bullet rather than to the main body itself. Forexample, it is preferred that said post have a diameter equal to or lessthan about ⅓ of the diameter of the main body of the bullet, and thatthe gas check preferably does not extend along any axial surface of themain body of the bullet.

As may be seen in FIG. 7A and enlarged FIGS. 7B-D, an internal lockingsystem 90 preferably resides on the inside surface of aperture 28 andpreferably also the outside surface of post 80. Locking, ridge 84protrudes inward toward the axis of the gas check from the peripheralwall of aperture 28. This locking ridge 84 assists in securing the gascheck 20 to the bullet 12, by frictional gripping or engaging of theback post 80 of the bullet 12. Preferably, back post 80 of the bullet 12has been provided with a cooperating radial indent, cannelure, orretaining ring 82. This way, the gas check 20 is more firmly secured tothe bullet 12, and vice-versa, so there is little chance that the gascheck and bullet will disconnect during loading or during carrying andhandling prior to firing. Consequently, when the projectile with the gascheck 20 of the present invention is seated in the bore of the barrel,in front of the powder charge, the bullet 12 will not easily separatefrom the gas check 20, and will not easily fall out of the barrel 14.Preferably the internal ridges are between about 0.001″ and 0.006″ high,and between about 0.001″ and 0.006″ wide.

FIGS. 7A and 7B illustrate a version of the internal locking system 90that includes a generally rectangular locking ridge 84 received in acurved, concave ring 82; thus, said ridge 84 and ring 82 do not exactlymatch in shape, but the ridge 84 is caught in ring 82 well enough toimprove the security of the gas check-to-bullet connection. FIG. 7Cillustrates an alternative version of an internal locking ridge system,wherein a rectangular ridge 84 is captured in a rectangular ring 86.FIG. 7D illustrates another alternative internal locking ridge system,wherein a wedge-shaped ridge 89 closely matches and mates with awedge-shaped ring 88. Many other styles, sizes, and numbers ofridges/rings may be used. For example, a slightly deeper groove at therearward portion of the ring may cooperate with a slightly longerextending portion of the internal radial ridge of the gas check at thatsame location; such a close and accurate mating may more firmly securedto the bullet, and vice-versa.

The preferred embodiments are made so that upon exiting the barrel, thegas check will disengage, detach, or break off of the bullet, orotherwise free the bullet. Rather than the entire gas check “popping”off of the bullet, for example, by means of aperture 28 disconnectingfrom the post 80, the preferred mechanism of detachment involves thefracture of the gas check member at one or more locations, under theforce of the gases rushing towards the uncapped distal end of the barrelor under the force of said gases and the sudden freeing of thegas-check-and-bullet combination from the barrel. For example, thefracture may occur at its forward end, along a connective band or“annular disk” between the engaging member and the outer skirt (forexample, ring 34, discussed below), and/or at one or more locations onthe outer skirt (for example, grooves 62, discussed below). The gascheck is preferably engineered to rupture along both said annular diskand a plurality of thin, scored, or otherwise weakened axial lines onthe outer skirt, such as grooves 62. Upon exiting the barrel, the skirtof the gas check separates from the bullet, and/or breaks into multiplepieces 123, allowing the bullet to continue, unimpeded, toward thetarget. See the schematic illustration in FIG. 8 of possible gas checkfracture upon leaving the muzzle loading firearm barrel.

Therefore, while the interior wall surface 25 of the skirt 23 may be ofvarious shapes, the preferred is a cylindrical wall with axial groovesrunning from at or near the rearmost end 64 of the skirt 23 to the ring34. There may be various numbers, sizes, and shapes of said axialgrooves, but it is preferred that there be 6-9 of said grooves spacedevenly around the circumference of the skirt 23 for symmetry of theskirt. These grooves 62 may serve to make the skirt 23 more flexible andexpandable for its purpose of sealing against the bore wall of thebarrel to capture the gases from the powder explosion. These grooves mayserve, in addition or instead, as weakened regions of the skirt forallowing the skirt to break apart at a desired time during the travel ofthe bullet and gas check, as discussed above. Preferably, immediatelyupon exit from the barrel, the skirt 23 will break off of the axial ring30 and/or will break apart at grooves 62, so that there is little ornone of the gas check left on the bullet as it travels beyond thebarrel. Note that, preferably, the interior surface 25 of the skirtcomprises no circumferential grooves or recesses, as this might weakenthe skirt in a direction that might allow axial compression (such as“accordion” collapsing of the skirt) or other deformation other than thepreferred slight radial expansion or flexing. Note that, preferably,there are no axial grooves or other breaks or indents in the externalridges (52/51, 53, 56/55), as these ridges should be circumferentiallycontinuous for sealing, with the bore all the way around the gas check.

Other connection means may be used to connect the gas check to thebullet. For example, the gas check may comprise a skirt extension thatextends forward from the shoulder S of the preferred gas check and alongthe bullet. This is not preferred, however, and tends not to benecessary, as the preferred light-weight gas check (simply connecting atthe pin and aperture connection and having a recess and ridge system) iseffective in bullet retention in the bore and gas capturing.

Other embodiments of the invention may also be made and used after oneof skill in the art reads this disclosure and views the drawings.Although this invention has been described above with reference toparticular means, materials and embodiments, it is to be understood thatthe invention is not limited to these disclosed particulars, but extendsinstead to all equivalents within the scope of the following claims.

1-18. (canceled)
 19. A gas check and muzzle loading bullet combination,comprising: a bullet having a back coupled to a gas check having arearwardly extending skirt including an external side wall surfaceadapted to contact a bore of a muzzle loading firearm and an interiorside wall surface; and an area formed in the interior side wall surfaceweakening the skirt.
 20. A gas check and muzzle loading bulletcombination according to claim 19, wherein the area comprises an axialgroove formed in the interior side wall surface.
 21. A gas check andmuzzle loading bullet combination according to claim 19, wherein thearea comprises axial grooves formed in the interior side wall surface.22. A gas check and muzzle loading bullet combination according to claim19, further comprising: a bullet post formed in the back of the bullet;and an aperture formed in the gas check receiving the bullet postcoupling the bullet to the gas check.
 23. A gas check and muzzle loadingbullet combination according to claim 19, further comprising theexternal side wall surface has a ridge and an adjacent recess to contactand to not contact, respectively, a bore of a muzzle loading firearm.24. A gas check for connection to a muzzle loading bullet, comprising: afront wall adapted to connect a bullet and an attached rearwardlyextending skirt including an external side wall surface adapted tocontact a bore of a muzzle loading firearm and an interior side wallsurface; and an area formed in the interior side wall surface weakeningthe skirt.
 25. A gas check according to claim 24, wherein the areacomprises an axial groove formed in the interior side wall surface. 26.A gas check according to claim 24, wherein the area comprises axialgrooves formed in the interior side wall surface.
 27. A gas checkaccording to claim 24, further comprising an aperture formed in thefront wall to receive and connect a bullet.
 28. A gas check according toclaim 24, further comprising the external side wall surface has a ridgeand an adjacent recess to contact and to not contact, respectively, abore of a muzzle loading firearm.